EASA Regulations &amp; Airworthiness Directives

Doors — Passenger Door Girt Bar Retention — Modification

EASA Airworthiness Directive 2019-0076 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It addresses the passenger door girt bar retention system to prevent dislodgement issues that could impair the functionality of the emergency evacuation slides. This directive applies to all manufacturer serial numbers of the Airbus A350-941 model.

Airbus A350941

EASA AD US-2019-06-07

Engine Fuel & Control - Fuel Nozzles and Supply Manifold Assemblies - Inspection / Replacement / Modification

The Federal Aviation Administration's Airworthiness Directive 2019-06-07 addresses certain Pratt & Whitney PW4164, PW4164-1D, PW4168, PW4168-1D, PW4168A, PW4168A-1D, and PW4170 turbofan engines. This directive mandates inspections and replacements related to fuel nozzles and fuel nozzle supply manifold assemblies to prevent fuel leaks associated with the Talon IIB combustion chamber configuration. It also requires installation of new brackets and clamps on the fuel nozzle supply manifold assemblies.

Pratt & Whitney PW4100

EASA AD 2019-0078

Flight Controls — Trimmable Horizontal Stabilizer Actuator Ball Nut Trunnion Lower Attachment — Inspection of Right-Hand Bearing Installation

EASA Airworthiness Directive 2019-0078 is an airworthiness directive addressing the inspection of the right-hand bearing installation on the trimmable horizontal stabilizer actuator ball nut trunnion lower attachment for Airbus A300, A300-600, A300-600ST, and A310 aeroplanes. It mandates a one-time detailed inspection of the affected parts to ensure proper installation and prevent potential actuator failure. The directive applies to all certified models and serial numbers of these Airbus aircraft.

Airbus A300600600ST (Beluga)600ST
Airbus A310

EASA AD 2019-0077

Standard Practices / Structures — Wing, Fuselage and Horizontal Stabilizer Fitting Bushings — Inspection / Replacement / Securing Modification

EASA Airworthiness Directive 2019-0077 is an airworthiness directive applicable to Allstar PZL Glider Sp. z o.o. SZD-54-2 “Perkoz” sailplanes with specific serial numbers. It addresses inspection, replacement, and securing modifications of wing, fuselage, and horizontal stabilizer fitting bushings to ensure continued airworthiness and safety of these sailplanes.

Allstar Pzl Glider SZD-54 Perkoz
Allstar PZL Glider SZD-54-2

EASA AD 2019-0075

Superseded by EASA AD 2019-0249

EASA Airworthiness Directive SUPERSEDED BY EASA AD 2019-0249 concerns Rolls-Royce Deutschland Ltd & Co KG Trent 1000 engines. This directive has been superseded and is no longer the current regulatory requirement. It originally addressed airworthiness issues related to the Trent 1000 engine model.

Rolls-Royce Deutschland Ltd & Co Kg TRENT 1000

EASA AD 2019-0071

Engine — Low Pressure Turbine Rear Support Seal Panel — Replacement

EASA Airworthiness Directive 2019-0071 is an airworthiness directive addressing Rolls-Royce Trent XWB-75, XWB-79, XWB-79B, and XWB-84 engines, commonly installed on Airbus A350 aircraft. The directive mandates the replacement of certain low pressure turbine rear support seal panel assemblies identified by specific serial numbers due to manufacturing defects. This action aims to maintain engine integrity and aircraft safety.

Rolls-Royce Deutschland Ltd & Co Kg TRENT XWB
Airbus A350

EASA AD RU-2017-322-05

NOT ADOPTED - EASA DECISION ATTACHED

EASA Decision not to adopt FATA AD 2017-322-05 is a regulatory decision concerning Sukhoi Civil Aircraft JSC RRJ-95 aeroplanes. The decision addresses the requirement for repetitive inspections of fuselage Frame 58 to detect cracks and the associated corrective actions. EASA concluded that the risk of undetected cracking is extremely low due to existing inspections and repair instructions provided by Sukhoi Civil Aircraft JSC.

Agency Decision

Irkut Corporation Jsc RRJ-95
Sukhoi RRJ-95

EASA AD 2018-0212R1

Powerplant — Engine Mount Titanium Crossbeam — Replacement [Life Limitation]

EASA Airworthiness Directive 2018-0212R1 is a regulatory document addressing the life limitation and replacement requirements for the forward engine mount titanium crossbeam, part number 238-0204-501, installed on Airbus A319-113, A319-114, A320-211, and A320-212 aeroplanes equipped with CFM56-5A engines. The directive mandates tracking the accumulated flight cycles of these crossbeams and replacing them before exceeding a life limit of 64,000 flight cycles to prevent potential failure and engine detachment in flight.

Airbus A319
Airbus A320

EASA AD 2019-0070

Stabilizers — Vertical Stabilizer Attachment Fittings — Inspection / Modification

EASA Airworthiness Directive 2019-0070 is an official regulatory document addressing inspection and modification requirements for the vertical stabilizer attachment fittings on DAHER AEROSPACE TBM 700 aeroplanes, specifically serial numbers 001 through 308 inclusive and 310. The directive mandates inspections for cracks caused by corrosion and provides instructions for optional modification using improved corrosion-resistant fittings. It applies to specific part numbers of vertical stabilizer attachment fittings and aims to maintain the structural integrity of the vertical stabilizer.

Daher Aerospace TBM 700

EASA AD US-2019-06-06

Superseded by FAA AD 2021-05-18

FAA Airworthiness Directive 2019-06-06 is a final rule addressing all International Aero Engines AG V2500 turbofan engine models. It mandates initial and repetitive borescope inspections of the diffuser case M-flange and requires replacement of the diffuser case if cracks are detected. This directive aims to prevent uncontained diffuser case rupture that could damage the engine and aircraft.

International Aero Engines Ag V2500-( )5
International Aero Engines Ag V2500-A1

EASA AD 2019-0073

Tail Rotor — Full Ice Protection System Tail Rotor Blades — Inspection / Replacement

EASA Airworthiness Directive 2019-0073 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Leonardo S.p.A. AB139 and AW139 helicopters equipped with the Full Ice Protection System (FIPS). It addresses inspection and replacement requirements for specific tail rotor blades with part numbers 4G6410A00131, 4G6410A00132, and 4G6410A00133. The directive aims to ensure the continued airworthiness of these helicopters by mitigating risks related to tail rotor blade damage.

Leonardo S.P.A. Helicopters AB139
Leonardo S.P.A. Helicopters AW139
Leonardo AB139
Leonardo AW139

EASA AD 2019-0072

Time Limits / Maintenance Checks – Airworthiness Limitations Section Part 2 – Damage Tolerant Airworthiness Limitation Items – Implementation

EASA Airworthiness Directive 2019-0072 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all Airbus A380-841, A380-842, and A380-861 aeroplanes. It mandates compliance with the Airbus A380 Airworthiness Limitations Section Part 2 Revision 07, which includes damage tolerant airworthiness limitation items. This directive ensures the continued airworthiness of these aircraft by requiring updated maintenance tasks and intervals.

Airbus A380841842861

EASA AD 2019-0065

Mar 27, 2019

Fuselage — Rear Fuselage Cone Diagonal Struts — Replacement

EASA Airworthiness Directive 2019-0065 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting Airbus A350-941 aeroplanes. It mandates the replacement of rear fuselage cone diagonal struts with new serviceable parts to ensure structural integrity. This directive applies to all serial numbers except those with Airbus modification 108588 incorporated during production.

Airbus A350941

EASA AD 2019-0066

Mar 27, 2019

Landing Gear — Nose Landing Gear Leg Assembly — Inspection

EASA Airworthiness Directive 2019-0066 is an airworthiness directive addressing the nose landing gear leg assembly inspection for Diamond Aircraft Industries GmbH DA 42, DA 42 M, DA 42 NG, and DA 42 M-NG aeroplanes. It mandates repetitive inspections of the nose landing gear actuator attachment lever to detect cracks that could lead to restricted rudder control. The directive applies to all serial numbers, including those converted via specific service bulletins.

Diamond Aircraft Industries DA 42
Diamond Aircraft Industries GmbH DA 42
Diamond Aircraft Industries GmbH DA 42 MNG
Diamond Aircraft Industries GmbH DA 42 NG

EASA AD 2019-0068

Mar 27, 2019

Nacelles / Pylons — Pylon Block Seals — Inspection / Replacement

EASA Airworthiness Directive 2019-0068 is an airworthiness directive issued by the European Union Aviation Safety Agency concerning Airbus A320-251N and A321-253N aeroplanes. It addresses cracks found in pylon block seals, specifically part numbers D0003167600000 and D0003167600100, which could compromise firewall integrity between the pylon and nacelle. The directive mandates inspection and replacement of these seals to ensure continued airworthiness.

Airbus A320251N
Airbus A321253N

EASA AD 2019-0063

Mar 26, 2019

Superseded by EASA AD 2019-0164

EASA Airworthiness Directive SUPERSEDED BY EASA AD 2019-0164 pertains to Airbus S.A.S. aircraft models A330 and A340. This directive has been officially replaced by EASA AD 2019-0164 and no longer applies as the active regulatory requirement. It originally addressed airworthiness concerns specific to these Airbus wide-body aircraft types.

Airbus A330
Airbus A340

EASA AD 2019-0062

Mar 26, 2019

Time Limits / Maintenance Checks – Airworthiness Limitations – Amendment

EASA Airworthiness Directive 2019-0062 is an airworthiness directive issued by the European Union Aviation Safety Agency affecting all serial numbers of PZL SW-4 helicopters. It mandates compliance with updated airworthiness limitations as specified in the PZL SW-4 Instructions for Continued Airworthiness - Maintenance Manual, Revision 14 dated November 2018. This directive ensures the continued airworthiness of these helicopters by enforcing maintenance tasks and life limits.

Wsk Pzl-Swidnik SW4
PZL SW-4

EASA AD US-2019-05-07

Mar 25, 2019

Engine - Compressor Fan Disks - Removal / Replacement

The Federal Register document titled "Engine - Compressor Fan Disks - Removal / Replacement" is a final rule Airworthiness Directive (AD 2019-05-07) issued by the FAA affecting certain Honeywell International Inc. TFE731 turbofan engines, specifically models TFE731-20R, -20AR, -20BR, -40AR, -40BR, and -40R. It addresses unsafe conditions related to fan disks with surface rollovers in the dovetail slot area. The AD mandates removal and replacement of affected fan disks to ensure continued airworthiness.

Honeywell International TFE731-20
Honeywell International -40
Honeywell International -50
Honeywell International -60

EASA AD 2019-0061

Mar 25, 2019

Engine – Power Turbine Disc – Inspection / Replacement

EASA Airworthiness Directive 2019-0061 is an airworthiness directive addressing certain GE Aviation Czech M601 series engines installed on various aircraft including the Aircraft Industries L-410 series, Air Tractor AT series, Allied Ag Cat G-164 series, PZL-106 Kruk, RUAG Do 28 series, and Thrush S-2R series. The directive mandates inspection and potential replacement of power turbine discs with specific part numbers and serial numbers to prevent failure due to damage or non-conforming geometry.

Ge Aviation Czech M601
Aircraft Industries L-410
Air Tractor AT
Allied Ag Cat G-164
PZL-106 Kruk
RUAG Do 28
Thrush S-2R

EASA AD 2019-0051R1

Mar 25, 2019

Superseded by EASA AD 2021-0039

EASA Airworthiness Directive 2019-0051R1 is an interim safety directive affecting all Boeing 737-8 and 737-9 MAX aircraft. It suspends normal flight operations of these models due to safety concerns following two fatal accidents and allows only limited ferry flights under strict conditions. The directive aims to ensure continued airworthiness pending further investigation and corrective actions.